Accession Number : ADA141341
Title : Base Pressure Measurements on a Projectile Shape at Mach Numbers from 0.91 to 1.20.
Descriptive Note : Final rept.,
Corporate Author : ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD
Personal Author(s) : Kayser,L D
PDF Url : ADA141341
Report Date : Apr 1984
Pagination or Media Count : 34
Abstract : Base pressure measurements were obtained on an axisymmetric projectile shape with and without a boattail. The tests were conducted in a transonic wind tunnel at Mach numbers of 0.91, 0.94, 0.96, 0.98, 1.10, and 1.20. Data were obtained at angles of attack of 0, 2, 3, 6, and 10 degrees and at circumferential positions around the model in 22.5 degree increments. Results were presented in both graphical and tabular form.
Descriptors : *Base pressure, *Projectiles, *Mach number, Transonic wind tunnels, Experimental data, Wind tunnel tests, Angle of attack, Boattail afterbodies, Aerodynamic forces, Ogives, Navier Stokes equations, Pressure measurement, Transonic characteristics, Axisymmetric, Coefficients, Aerodynamic drag
Subject Categories : Test Facilities, Equipment and Methods
Ammunition and Explosives
Distribution Statement : APPROVED FOR PUBLIC RELEASE